Y 3.N 21/5:8/1317
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A simple numerical method for the calculation of the laminar boundary layer / |
1 |
Y 3.N 21/5:8/1318
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Friction and wear / |
1 |
Y 3.N 21/5:8/1319
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Torsion and bending of prismatic rods of hollow rectangular section / |
1 |
Y 3.N 21/5:8/1320
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Investigations on wings with and without sweepback at high subsonic speeds / |
1 |
Y 3.N 21/5:8/1321
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Relations between the modulus of elasticity of binary alloys and their structure / |
1 |
Y 3.N 21/5:8/1322
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Theory of thin-walled rods / |
1 |
Y 3.N 21/5:8/1323
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Influence of static longitudinal stability on the behavior of airplanes in gusts / |
1 |
Y 3.N 21/5:8/1324
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Steady vibrations of wing of circular plan form : and Theory of wing of circular plan form / |
1 |
Y 3.N 21/5:8/1325
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Concerning the flow about ring-shaped cowlings of finite thickness. : Part 1 / |
1 |
Y 3.N 21/5:8/1326
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Concerning the flow about ring-shaped cowlings. : Part 2 - Annular bodies of infinite length with circulation for smooth entrance / |
1 |
Y 3.N 21/5:8/1327
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Concerning the flow about ring-shaped cowlings. : Part 6 - Further measurements on inlet devices / |
1 |
Y 3.N 21/5:8/1328
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Concerning the flow about ring-shaped cowlings. : Part 8 - Further measurements on annular profiles / |
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Y 3.N 21/5:8/1329
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Concerning the flow about ring-shaped cowlings. : Part 9 - The influence of oblique oncoming flow on the incremental velocities and air forces at the front part of circular cowls / |
1 |
Y 3.N 21/5:8/1330
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Theory of dynamic creep / |
1 |
Y 3.N 21/5:8/1331
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Investigations of the boundary-layer control on a full scale swept wing with air bled off from the turbojet / |
1 |
Y 3.N 21/5:8/1332
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Extension to the cases of two dimensional and spherically symmetric flows of two particular solutions to the equations of motion governing unsteady flow in a gas / |
1 |
Y 3.N 21/5:8/1333
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On rotational conical flow / |
1 |
Y 3.N 21/5:8/1334
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The effect of high viscosity on the flow around a cylinder and around a sphere / |
1 |
Y 3.N 21/5:8/1335
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Motion of a cylinder under the surface of a heavy fluid / |
1 |
Y 3.N 21/5:8/1336
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Development of a laminar boundary layer behind a suction point / |
1 |